The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …

Time-resolved CH* chemiluminescence imaging was performed at 50 kHz in order to study
flame motion and stabilization in the axial flow direction in a dual-mode scramjet at the …

The extended phase-consistent dynamic mode decomposition (DMD) method, which
reconstructs density fields from density gradient fields in multiple directions, was developed …

This study investigates the flow field induced by a surface dielectric barrier discharge
(SDBD) system, known for its efficient pollution remediation of volatile organic compounds …

The unexpected release of hazardous gases due to natural/industrial accidents or man-
made disasters can have tragic consequences. Compared with other gaseous pollutants …

A high-speed flow visualisation set-up comprising of combined diffuse backlight illumination
(DBI) and schlieren imaging has been developed to illustrate the highly transient, two-phase …

Hysteresis in flame stabilization mode transitions in a hydrogen-fueled strut-stabilized
supersonic combustion test rig was experimentally observed and studied. Air was vitiated …

A method for measuring planar temperature fields of fluid flows is proposed. The focusing
schlieren technique together with a calibration procedure to fulfill such a purpose is used …

The flow around a hypersonic vehicle is characterised by certain physical flow phenomena,
eg viscous interaction, high-temperature effects, etc., and the resulting high heat load …

This paper presents a focusing schlieren system designed for the investigation of transonic
turbine tip-leakage flows. In the first part, the functional principle and the design of the …